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Journal Articles Aerospace Lab Year : 2014

An analysis of shock noise components


Screech and broadband shock-associated noise linked to the presence of a shockcell structure in supersonic jets are reviewed in this paper. Only underexpanded supersonic circular jets issued from a convergent nozzle are considered here. An overview of the flow and of these two noise components is presented, based on recent experimental and numerical work. Flight effects on broadband shock-associated noise are also introduced, within the framework of aeronautical applications.


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hal-01184727 , version 1 (17-08-2015)



C. Bailly, B. André, T. Castelain, C. Henry, G. Bodard, et al.. An analysis of shock noise components. Aerospace Lab, 2014, 7, p. 1-8. ⟨10.12762/2014.AL07-06⟩. ⟨hal-01184727⟩
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